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Autore: |
Csank Jeffrey T.
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Titolo: |
A turbine based combined cycle engine inlet model and mode transition simulation based on HiTECC tool / / Jeffrey T. Csank and Thomas J. Stueber
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Pubblicazione: | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2012 |
Descrizione fisica: | 1 online resource (13 pages) : color illustrations |
Soggetto topico: | Computerized simulation |
Propulsion system configurations | |
Wind tunnel tests | |
Fuel systems | |
Propulsion system performance | |
Turbine engines | |
Engine inlets | |
Persona (resp. second.): | StueberThomas J. |
Note generali: | Title from title screen (viewed on Jan. 14, 2013). |
"September 2012." | |
"Prepared for the 48th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE Atlanta, Georgia, July 30 to August 1, 2012." | |
"AIAA-2012-4149." | |
Nota di bibliografia: | Includes bibliographical references (pages 12-13). |
Titolo autorizzato: | A turbine based combined cycle engine inlet model and mode transition simulation based on HiTECC tool ![]() |
Formato: | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione: | Inglese |
Record Nr.: | 9910702486003321 |
Lo trovi qui: | Univ. Federico II |
Opac: | Controlla la disponibilità qui |